自旋稳定卫星海上测控姿章联控及实现  

The Implementation of Attitude & Nutation United Control for Slow-roll Stabilization Satellite's Maritime Tracking and Control

作　　者：柏文良[1] 顾炳俊[1] 朱加勇[1] 徐贵斌[1] 王瑞东[1] 施宇星[1] 

机构地区：[1]中国卫星海上测控部,江苏江阴214431

出　　处：《上海航天》2007年第5期58-61,共4页Aerospace Shanghai

摘　　要：介绍了同步轨道自旋稳定卫星海上姿态章动联合控制原理。通过分析等倾角进动过程,建立了理论与实际执行角、同步脉冲执行次数和时延的计算模型,并给出了姿章联控系统的组成及实现过程。The principle of united control of attitude ＆ nutation in maritime tracking and control for slow-roll stabilization satellite was introduced in this paper. The process with equal precession angle was analyzed. The computation modes of theory and real actuating angle, actuating times of synchronous pulse, and time relay were established. The constitution and implementation procedure of the united control of attitude ＆ nutation system were also presented.

关 键 词：自旋稳定卫星 海上测控 姿章联控遥 测遥控处理机 同步控制器 同步控制参数 

分 类 号：V556[航空宇航科学与技术—人机与环境工程]